US20050188945A1 - Method and apparatus for adjusting fuel injection timing - Google Patents

Method and apparatus for adjusting fuel injection timing Download PDF

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Publication number
US20050188945A1
US20050188945A1 US10/787,991 US78799104A US2005188945A1 US 20050188945 A1 US20050188945 A1 US 20050188945A1 US 78799104 A US78799104 A US 78799104A US 2005188945 A1 US2005188945 A1 US 2005188945A1
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Prior art keywords
timing
fuel injection
offset
injection timing
change
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US7093579B2 (en
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Steven Dickerson
James Beaucaire
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JPMorgan Chase Bank NA
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Priority to US10/787,991 priority Critical patent/US7093579B2/en
Assigned to INTERNATINAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC reassignment INTERNATINAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BEAUCAIRE, JAMES T., DICKERSON, STEVEN J.
Priority to BRPI0508070-3A priority patent/BRPI0508070A/en
Priority to PCT/US2005/004255 priority patent/WO2005081806A2/en
Priority to CNB2005800055982A priority patent/CN100451319C/en
Priority to CA2553876A priority patent/CA2553876C/en
Priority to EP05713288A priority patent/EP1725753A4/en
Priority to KR1020067017158A priority patent/KR20060129031A/en
Priority to JP2007500857A priority patent/JP2007525614A/en
Publication of US20050188945A1 publication Critical patent/US20050188945A1/en
Publication of US7093579B2 publication Critical patent/US7093579B2/en
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Assigned to JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT reassignment JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT SECURITY AGREEMENT Assignors: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION, NAVISTAR, INC.
Assigned to JPMORGAN CHASE BANK N.A., AS COLLATERAL AGENT reassignment JPMORGAN CHASE BANK N.A., AS COLLATERAL AGENT SECURITY AGREEMENT Assignors: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION
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Assigned to NAVISTAR, INC., INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION reassignment NAVISTAR, INC. RELEASE BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
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Assigned to JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT reassignment JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT CORRECTIVE ASSIGNMENT TO CORRECT THE CONVEYING PARTY DATA PREVIOUSLY RECORDED AT REEL: 052483 FRAME: 0742. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY INTEREST.. Assignors: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION, NAVISTAR, INC. (F/K/A INTERNATIONAL TRUCK AND ENGINE CORPORATION)
Assigned to THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT reassignment THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION, NAVISTAR, INC. (F/K/A INTERNATIONAL TRUCK AND ENGINE CORPORATION)
Assigned to INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR, INC. (F/KA/ INTERNATIONAL TRUCK AND ENGINE CORPORATION) reassignment INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC RELEASE BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Assigned to NAVISTAR, INC., INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC, INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC, NAVISTAR INTERNATIONAL CORPORATION reassignment NAVISTAR, INC. RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 53545/443 Assignors: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/40Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/401Controlling injection timing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/40Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3011Controlling fuel injection according to or using specific or several modes of combustion
    • F02D41/3017Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3011Controlling fuel injection according to or using specific or several modes of combustion
    • F02D41/3064Controlling fuel injection according to or using specific or several modes of combustion with special control during transition between modes
    • F02D41/307Controlling fuel injection according to or using specific or several modes of combustion with special control during transition between modes to avoid torque shocks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/40Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/402Multiple injections
    • F02D41/403Multiple injections with pilot injections
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

Definitions

  • the present invention relates to internal combustion engines, including but not limited to fuel injection systems that use multiple injections of fuel into a combustion chamber of an engine.
  • Multiple injections of fuel may be accomplished by either multiple fuel injectors or by a single fuel injector that is constructed and operated to allow for multiple injections.
  • multiple injections of fuel include a pilot and a main injection.
  • the relative volume of the pilot and main injections may differ considerably.
  • the pilot injection is small in volume compared to a volume of the main injection.
  • the timing of fuel injection for desired engine performance depends on whether the engine is operating with or without pilot injections. Switching pilot injection on or off can affect engine performance. For example, engine roughness often occurs when engine operation is changed by adding or removing pilot fuel injection to a main fuel injection.
  • a method of adjusting fuel injection timing comprises the steps of detecting a change in a number of fuel injections into a combustion chamber of an internal combustion engine, and in response to detection of the change, determining a timing adjustment period. During the timing adjustment period, the fuel injection timing is adjusted.
  • FIG. 1 shows an internal combustion engine having a fuel injection system in accordance with the invention.
  • FIG. 2 illustrates a logic diagram for use with a fuel injection system in accordance with the invention.
  • FIG. 3 is a graph illustrating various timing offsets versus time in accordance with the invention.
  • FIG. 4 is a flowchart illustrating a method of fuel injection timing adjustment in accordance with the invention.
  • the following describes a method and apparatus for adjusting fuel injection timing when a change in the number of fuel injections for a combustion chamber is detected.
  • the timing for fuel injection(s) may be adjusted incrementally, e.g., in a series of steps or increments, and/or based at least in part on the time elapsed since the detected of the change in the number of fuel injections.
  • FIG. 1 An internal combustion engine 100 having a fuel injection system is shown in FIG. 1 .
  • An engine control module (ECM) 101 controls one or more fuel injectors 103 of the engine 100 .
  • the engine 100 shown comprises one or more combustion chambers 105 , pistons 107 , cylinders 109 , inlet valves 111 , outlet valves 113 , and connecting rods 123 , in addition to a crankshaft 117 , a flywheel 115 , engine speed sensor 119 , and/or an accelerator pedal sensor 121 arranged to operate as known in the art.
  • One or more fuel injections are injected into the combustion chamber 105 during each engine cycle.
  • injections may comprise a pilot injection and a main injection, as known in the art.
  • a fuel injection event may comprise a main injection only, a pilot injection and a main injection, multiple pilot injections, and a main injection, as well as other combinations in various numbers of injections.
  • Single or multiple injections of fuel may be selected depending on desired engine operation and performance.
  • the ECM 101 may include one or more microprocessors that control the operation of the fuel injection system and/or various other functions of the engine 100 .
  • the ECM 101 may provide control of the number of fuel injections, the timing of each of the one or more fuel injections, the amount of each fuel injection, and so forth.
  • the ECM 101 may select single or multiple fuel injections based on engine load or torque.
  • the ECM 101 may determine or adjust fuel injection timing based on ECM programming, inputs from engine or vehicle sensors 119 or 121 , and so forth.
  • Fuel injection timing is typically measured in degrees relative to when the piston 107 is at a top dead center position in the cylinder 109 .
  • the ECM 101 may adjust fuel injection timing.
  • the adjustment may be a combination of one or more offsets.
  • a logic diagram for use with a fuel injection system is shown in FIG. 2 .
  • the logic may be implemented, for example, in a computer program that is executed by the ECM 101 and/or another processor that controls fuel injection timing.
  • the fuel injection system is considered to operate in one of two modes.
  • Mode 1 occurs when fuel injection timing adjustments are made to account for a change in the number of fuel injections, for example, between consecutive fuel injection events.
  • a change in the number of fuel injections occurs, for example, when a change is made from main injection only to main plus pilot injection, from main plus pilot injection to main injection only, from main plus N pilot injections to main plus M pilot injections, where N is not equal to M, and so forth.
  • Mode 1 lasts for a period of time that is referred to as a timing adjustment period.
  • Mode 0 refers to steady state operation, when no fuel injection timing adjustment is made to compensate for a change in the number of fuel injections in a given engine cycle, which fuel injection timing is referred to as steady state fuel injection timing.
  • a timer 201 is started.
  • the change in mode from 0 to 1 indicated a detected change in the number of fuel injections for an engine cycle.
  • the output of the timer 201 indicates the elapsed time since the detection of a change in the number of fuel injections.
  • the timer 201 is set for a time equal to the timing adjustment period. When the elapsed time of the timer 201 reaches the timing adjustment period, the mode changes from 1 to 0.
  • the output of the timer 201 is input to a converter 203 that converts the elapsed time into a multiplier.
  • the multiplier may advantageously take on a value between 0 and 1. Other ranges of values for the multiplier may also be utilized.
  • the multiplier is advantageously based at least in part on the time that has elapsed since the change in the number of fuel injections. Alternatively, the number of combustion cycles since the mode change may be used to calculate the multiplier at least in part.
  • the converter 203 may be calibrated for a particular type of engine by correlating engine test data. For example, engine tests that determine fuel injection timing that reduce or eliminate engine roughness when changing the number of fuel injections may be used to calibrate the converter 203 . The engine tests results may be used to determine a mathematical relationship that uses elapsed time as a variable to calculate the multiplier.
  • the multiplier is input to a combiner 205 .
  • the combiner combines the multiplier with a timing offset yielding a modified offset.
  • the multiplier is advantageously multiplied by the timing offset, in which case the combiner acts as a multiplier.
  • the multiplier may be a factor that is added to or subtracted from the timing offset by the combiner 205 .
  • Other methods of combining may be utilized.
  • the timing offset may be, for example, pilot injection timing offset or main injection timing offset. If, for example, pilot injection timing was activated causing the change in the number of fuel injections, the timing offset input into the combiner 205 is pilot injection timing offset. Main injection follows pilot injection as desired in time. If, for example, pilot injection timing was deactivated causing the change in the number of fuel injections, the timing offset input into the combiner 205 is main injection timing offset.
  • the timing offset may be determined in any number of ways. For example, a determine 211 having engine speed and change in engine load as inputs may be utilized to determine the timing offset.
  • the modified offset from the combiner 205 is input to a switch or multiplexer 207 .
  • the output of the switch 207 is controlled by the mode.
  • the mode i.e., steady state operation
  • the fuel injection timing offset related to change in the number of fuel injections is 0, and 0 is output by the switch 207 .
  • the mode is 1, the modified offset is output by the switch 207 .
  • a combiner 209 combines the output of the switch 207 , i.e., fuel injection timing offset related to change in the number of fuel injections, with other fuel injection timing factors as the fuel injection system may utilize. These factors may include, for example, timing adjustments for low or high altitude, oil temperature, transient to cruise engine operation, air temperature, engine speed, and so forth.
  • the combiner 209 outputs adjusted fuel injection timing that is utilized to control fuel injections.
  • FIG. 3 A graph illustrating various timing offsets versus time is shown in FIG. 3 .
  • time equals 0.0 seconds when the mode switches from 0 to 1
  • the x-axis values denote the time elapsed since the mode change, i.e., since the number of fuel injections changed.
  • the curves 301 , 303 , 305 , and 307 are shown for engine conditions of constant engine speed and load.
  • the solid curve 301 illustrates the typical implementation of prior art solutions when, for example, pilot injection is added to a main injection.
  • Fuel injection timing changes almost instantaneously from 0.0 degrees before top dead center (BTDC) to 6.0 degrees BTDC, the desired timing for the pilot injection.
  • Engine roughness or stumbling may occur with such a quick change in state from no pilot injection to having a pilot injection.
  • Three curves 303 , 305 , and 307 illustrate three different curves of modified offsets, as described with respect to FIG. 2 . Any number curves having other shapes than those shown may be utilized to achieve desired results.
  • the curves 303 , 305 , and 307 shown in the example of FIG. 3 may be utilized when the number of fuel injections increases, for example, when pilot injection is activated or added to main injection or when the number of pilot injections increases.
  • the sharpest curve 303 has the shortest timing adjustment period, less than 1.2 seconds.
  • the middle curve 305 has a 1.8 second timing adjustment period.
  • the most gradual curve 307 has the longest timing adjustment period of 2.2 seconds.
  • One of the curves 303 , 305 , and 307 may be utilized during a single timing adjustment period. During this period, each time a cylinder fires, the modified timing offset associated with the firing is determined from the curve by the time at which cylinder fires. If the cylinder fires at 0.4 seconds and curve 303 is utilized, the modified timing offset is approximately 3.5 degrees BTDC. As time passes, the modified timing offset incrementally or in steps increases until the target, or steady state timing, is achieved.
  • two or more of the curves may be utilized during a single timing adjustment period.
  • a cylinder firing at 0.4 seconds may utilize a timing offset of 0.2 degrees BTDC from the gradual curve 307
  • a cylinder firing at 0.6 seconds may utilize a timing offset of 2.5 degrees BTDC from the middle curve 305
  • a cylinder firing at 0.8 seconds may utilize a timing offset of 5.2 degrees BTDC from the sharp curve 303 .
  • Such a progression may be made based on current operating conditions.
  • the curves 303 , 305 , and 307 are implemented in the converter 203 . Similar curves that, for example, mirror the curves 303 , 305 , and 307 along the x-axis may be utilized to adjust timing when pilot injection is deactivated or the number of pilot injections is decreased, to decrease timing from, for example, 6.0 degrees BTDC to 0.0 degrees BTDC as time passes.
  • FIG. 4 A flowchart illustrating a method of fuel injection timing adjustment is shown in FIG. 4 .
  • step 401 it is determined whether a change in the number of fuel injections has occurred. If no change is detected, the process continues to attempt to detect such a change at step 401 .
  • step 403 the timing adjustment period is determined.
  • the timing adjustment period may be selected, thereby establishing the timing curves 303 , 305 , and 307 .
  • the timing curves 303 , 305 , and 307 may be selected, thereby establishing the timing adjustment period.
  • the timing adjustment period begins when the mode changes from 0 to 1, although a delay may implemented.
  • step 405 fuel injection timing is adjusted as described with respect to FIG. 2 until the timing adjustment period ends at step 407 , and the process continues with step 401 . When the timing adjustment period ends, the mode changes from 1 to 0.
  • the present invention is illustrated by the example of a single cylinder of a diesel engine, the present invention may be applied to: engines having one or more cylinders; various engine types, such as in-line, V type, and so forth; engines having different cylinder firing orders; diesel engines, gasoline engines, or other types, of engines; turbocharged and non-turbocharged engines; engines of any size; and engines having fuel injectors that are capable of delivering two or more injections of fuel into the combustion chamber of the engine during an engine cycle.
  • the present invention provides a number of advantages.
  • Engine stumble or rough engine operation is reduced during transitions in engine operation to and from multiple fuel injection operation. Smoother, more reliable and efficient engine operation and vehicle performance result, and vehicle drivability and engine sociability improve.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

A method and apparatus for adjusting fuel injection timing detects (401) a change in the number of fuel injections for a combustion chamber (105). During a timing adjustment period, the timing for fuel injection(s) may be adjusted (405) incrementally, e.g., in a series of steps or increments, and/or based at least in part on the time elapsed since the detected of the change in the number of fuel injections.

Description

    FIELD OF THE INVENTION
  • The present invention relates to internal combustion engines, including but not limited to fuel injection systems that use multiple injections of fuel into a combustion chamber of an engine.
  • BACKGROUND OF INVENTION
  • Internal combustion engines are known to operate with single or multiple injections of fuel into a combustion chamber of the engine. Multiple injections of fuel may be accomplished by either multiple fuel injectors or by a single fuel injector that is constructed and operated to allow for multiple injections. Typically, multiple injections of fuel include a pilot and a main injection. The relative volume of the pilot and main injections may differ considerably. Generally, the pilot injection is small in volume compared to a volume of the main injection.
  • The timing of fuel injection for desired engine performance depends on whether the engine is operating with or without pilot injections. Switching pilot injection on or off can affect engine performance. For example, engine roughness often occurs when engine operation is changed by adding or removing pilot fuel injection to a main fuel injection.
  • Accordingly, there is to eliminate engine performance problems related to the activation or deactivation of pilot injection in the fuel injection process.
  • SUMMARY OF INVENTION
  • A method of adjusting fuel injection timing comprises the steps of detecting a change in a number of fuel injections into a combustion chamber of an internal combustion engine, and in response to detection of the change, determining a timing adjustment period. During the timing adjustment period, the fuel injection timing is adjusted.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 shows an internal combustion engine having a fuel injection system in accordance with the invention.
  • FIG. 2 illustrates a logic diagram for use with a fuel injection system in accordance with the invention.
  • FIG. 3 is a graph illustrating various timing offsets versus time in accordance with the invention.
  • FIG. 4 is a flowchart illustrating a method of fuel injection timing adjustment in accordance with the invention.
  • DESCRIPTION OF A PREFERRED EMBODIMENT
  • The following describes a method and apparatus for adjusting fuel injection timing when a change in the number of fuel injections for a combustion chamber is detected. During a timing adjustment period, the timing for fuel injection(s) may be adjusted incrementally, e.g., in a series of steps or increments, and/or based at least in part on the time elapsed since the detected of the change in the number of fuel injections.
  • An internal combustion engine 100 having a fuel injection system is shown in FIG. 1. An engine control module (ECM) 101 controls one or more fuel injectors 103 of the engine 100. The engine 100 shown comprises one or more combustion chambers 105, pistons 107, cylinders 109, inlet valves 111, outlet valves 113, and connecting rods 123, in addition to a crankshaft 117, a flywheel 115, engine speed sensor 119, and/or an accelerator pedal sensor 121 arranged to operate as known in the art.
  • One or more fuel injections are injected into the combustion chamber 105 during each engine cycle. When multiple injections are delivered, such injections may comprise a pilot injection and a main injection, as known in the art. A fuel injection event may comprise a main injection only, a pilot injection and a main injection, multiple pilot injections, and a main injection, as well as other combinations in various numbers of injections. Single or multiple injections of fuel may be selected depending on desired engine operation and performance.
  • The ECM 101 may include one or more microprocessors that control the operation of the fuel injection system and/or various other functions of the engine 100. The ECM 101 may provide control of the number of fuel injections, the timing of each of the one or more fuel injections, the amount of each fuel injection, and so forth. The ECM 101 may select single or multiple fuel injections based on engine load or torque. The ECM 101 may determine or adjust fuel injection timing based on ECM programming, inputs from engine or vehicle sensors 119 or 121, and so forth.
  • Fuel injection timing is typically measured in degrees relative to when the piston 107 is at a top dead center position in the cylinder 109. The ECM 101 may adjust fuel injection timing. The adjustment may be a combination of one or more offsets.
  • A logic diagram for use with a fuel injection system is shown in FIG. 2. The logic may be implemented, for example, in a computer program that is executed by the ECM 101 and/or another processor that controls fuel injection timing. The fuel injection system is considered to operate in one of two modes. Mode 1 occurs when fuel injection timing adjustments are made to account for a change in the number of fuel injections, for example, between consecutive fuel injection events. A change in the number of fuel injections occurs, for example, when a change is made from main injection only to main plus pilot injection, from main plus pilot injection to main injection only, from main plus N pilot injections to main plus M pilot injections, where N is not equal to M, and so forth. Mode 1 lasts for a period of time that is referred to as a timing adjustment period. Mode 0 refers to steady state operation, when no fuel injection timing adjustment is made to compensate for a change in the number of fuel injections in a given engine cycle, which fuel injection timing is referred to as steady state fuel injection timing.
  • When the mode changes from 0 to 1, a timer 201 is started. The change in mode from 0 to 1 indicated a detected change in the number of fuel injections for an engine cycle. The output of the timer 201 indicates the elapsed time since the detection of a change in the number of fuel injections. The timer 201 is set for a time equal to the timing adjustment period. When the elapsed time of the timer 201 reaches the timing adjustment period, the mode changes from 1 to 0.
  • The output of the timer 201 is input to a converter 203 that converts the elapsed time into a multiplier. The multiplier may advantageously take on a value between 0 and 1. Other ranges of values for the multiplier may also be utilized. The multiplier is advantageously based at least in part on the time that has elapsed since the change in the number of fuel injections. Alternatively, the number of combustion cycles since the mode change may be used to calculate the multiplier at least in part. The converter 203 may be calibrated for a particular type of engine by correlating engine test data. For example, engine tests that determine fuel injection timing that reduce or eliminate engine roughness when changing the number of fuel injections may be used to calibrate the converter 203. The engine tests results may be used to determine a mathematical relationship that uses elapsed time as a variable to calculate the multiplier.
  • The multiplier is input to a combiner 205. The combiner combines the multiplier with a timing offset yielding a modified offset. As shown in FIG. 2, the multiplier is advantageously multiplied by the timing offset, in which case the combiner acts as a multiplier. Alternatively, the multiplier may be a factor that is added to or subtracted from the timing offset by the combiner 205. Other methods of combining may be utilized.
  • The timing offset may be, for example, pilot injection timing offset or main injection timing offset. If, for example, pilot injection timing was activated causing the change in the number of fuel injections, the timing offset input into the combiner 205 is pilot injection timing offset. Main injection follows pilot injection as desired in time. If, for example, pilot injection timing was deactivated causing the change in the number of fuel injections, the timing offset input into the combiner 205 is main injection timing offset. The timing offset may be determined in any number of ways. For example, a determine 211 having engine speed and change in engine load as inputs may be utilized to determine the timing offset.
  • The modified offset from the combiner 205 is input to a switch or multiplexer 207. The output of the switch 207 is controlled by the mode. When the mode is 0, i.e., steady state operation, the fuel injection timing offset related to change in the number of fuel injections is 0, and 0 is output by the switch 207. When the mode is 1, the modified offset is output by the switch 207. A combiner 209 combines the output of the switch 207, i.e., fuel injection timing offset related to change in the number of fuel injections, with other fuel injection timing factors as the fuel injection system may utilize. These factors may include, for example, timing adjustments for low or high altitude, oil temperature, transient to cruise engine operation, air temperature, engine speed, and so forth. The combiner 209 outputs adjusted fuel injection timing that is utilized to control fuel injections.
  • A graph illustrating various timing offsets versus time is shown in FIG. 3. For the sake of simplicity, time equals 0.0 seconds when the mode switches from 0 to 1, and the x-axis values denote the time elapsed since the mode change, i.e., since the number of fuel injections changed. Also for the sake of simplicity, the curves 301, 303, 305, and 307 are shown for engine conditions of constant engine speed and load.
  • The solid curve 301 illustrates the typical implementation of prior art solutions when, for example, pilot injection is added to a main injection. Fuel injection timing changes almost instantaneously from 0.0 degrees before top dead center (BTDC) to 6.0 degrees BTDC, the desired timing for the pilot injection. Engine roughness or stumbling may occur with such a quick change in state from no pilot injection to having a pilot injection.
  • Three curves 303, 305, and 307 illustrate three different curves of modified offsets, as described with respect to FIG. 2. Any number curves having other shapes than those shown may be utilized to achieve desired results. The curves 303, 305, and 307 shown in the example of FIG. 3 may be utilized when the number of fuel injections increases, for example, when pilot injection is activated or added to main injection or when the number of pilot injections increases. The sharpest curve 303 has the shortest timing adjustment period, less than 1.2 seconds. The middle curve 305 has a 1.8 second timing adjustment period. The most gradual curve 307 has the longest timing adjustment period of 2.2 seconds.
  • One of the curves 303, 305, and 307 may be utilized during a single timing adjustment period. During this period, each time a cylinder fires, the modified timing offset associated with the firing is determined from the curve by the time at which cylinder fires. If the cylinder fires at 0.4 seconds and curve 303 is utilized, the modified timing offset is approximately 3.5 degrees BTDC. As time passes, the modified timing offset incrementally or in steps increases until the target, or steady state timing, is achieved.
  • Alternatively, two or more of the curves may be utilized during a single timing adjustment period. For example, a cylinder firing at 0.4 seconds may utilize a timing offset of 0.2 degrees BTDC from the gradual curve 307, a cylinder firing at 0.6 seconds may utilize a timing offset of 2.5 degrees BTDC from the middle curve 305, and a cylinder firing at 0.8 seconds may utilize a timing offset of 5.2 degrees BTDC from the sharp curve 303. Such a progression may be made based on current operating conditions.
  • The curves 303, 305, and 307 are implemented in the converter 203. Similar curves that, for example, mirror the curves 303, 305, and 307 along the x-axis may be utilized to adjust timing when pilot injection is deactivated or the number of pilot injections is decreased, to decrease timing from, for example, 6.0 degrees BTDC to 0.0 degrees BTDC as time passes.
  • A flowchart illustrating a method of fuel injection timing adjustment is shown in FIG. 4. At step 401, it is determined whether a change in the number of fuel injections has occurred. If no change is detected, the process continues to attempt to detect such a change at step 401. When a change is detected at step 401, the process continues with step 403, where the timing adjustment period is determined. The timing adjustment period may be selected, thereby establishing the timing curves 303, 305, and 307. Alternatively, the timing curves 303, 305, and 307 may be selected, thereby establishing the timing adjustment period. The timing adjustment period begins when the mode changes from 0 to 1, although a delay may implemented. At step 405, fuel injection timing is adjusted as described with respect to FIG. 2 until the timing adjustment period ends at step 407, and the process continues with step 401. When the timing adjustment period ends, the mode changes from 1 to 0.
  • Although the present invention is illustrated by the example of a single cylinder of a diesel engine, the present invention may be applied to: engines having one or more cylinders; various engine types, such as in-line, V type, and so forth; engines having different cylinder firing orders; diesel engines, gasoline engines, or other types, of engines; turbocharged and non-turbocharged engines; engines of any size; and engines having fuel injectors that are capable of delivering two or more injections of fuel into the combustion chamber of the engine during an engine cycle.
  • The present invention provides a number of advantages. Engine stumble or rough engine operation is reduced during transitions in engine operation to and from multiple fuel injection operation. Smoother, more reliable and efficient engine operation and vehicle performance result, and vehicle drivability and engine sociability improve.
  • The present invention may be embodied in other specific forms without departing from its spirit or essential characteristics. The described embodiments are to be considered in all respects only as illustrative and not restrictive. The scope of the invention is, therefore, indicated by the appended claims rather than by the foregoing description. All changes that come within the meaning and range of equivalency of the claims are to be embraced within their scope.

Claims (20)

1. A method comprising the steps of:
detecting a change in a number of fuel injections into a combustion chamber of an internal combustion engine;
determining a timing adjustment period that begins when the change is detected;
during the timing adjustment period, adjusting fuel injection timing.
2. The method of claim 1, wherein the step of adjusting comprises the step of incrementally adjusting the fuel injection timing based at least in part on an elapsed time from the detecting step.
3. The method of claim 1, wherein the step of detecting comprises detecting one of activation and deactivation of pilot fuel injection.
4. The method of claim 1, wherein the step of adjusting comprises adjusting main fuel injection timing.
5. The method of claim 1, wherein the step of adjusting comprises adjusting pilot fuel injection timing.
6. The method of claim 1, wherein the step of adjusting comprises:
determining a timing offset;
determining a multiplier based at least in part on the time elapsed since the detection of change;
combining the timing offset with the multiplier, yielding a modified offset;
utilizing the modified offset to adjust fuel injection timing.
7. A method comprising the steps of:
detecting a change in a number of fuel injections into a combustion chamber of an internal combustion engine;
determining a timing adjustment period;
during the timing adjustment period, adjusting fuel injection timing incrementally based at least in part on time elapsed since the detection.
8. The method of claim 7, wherein the step of detecting comprises detecting one of activation and deactivation of pilot fuel injection.
9. The method of claim 7, wherein the step of adjusting comprises:
determining a timing offset;
determining a multiplier based at least in part on the time elapsed since the detection;
combining the timing offset with the multiplier, yielding a modified offset;
utilizing the modified offset to adjust fuel injection timing.
10. The method of claim 9, wherein the timing offset is based on at least one of engine speed and change in engine load.
11. The method of claim 9, wherein as time progresses, the multiplier is stepped incrementally between timing at detection of the change and steady state timing.
12. The method of claim 9, wherein the multiplier gradually changes during the timing adjustment period.
13. The method of claim 9, wherein the timing offset is a pilot injection timing offset.
14. The method of claim 9, wherein the timing offset is a main injection timing offset.
15. An apparatus comprising:
an engine control module arranged and constructed to detect a change from a first number to a second number of fuel injections into a combustion chamber of an internal combustion engine, to determine a timing adjustment period, and to adjust fuel injection timing during the timing adjustment period;
wherein the engine control module is operable with a fuel injection system capable of providing the first number and the second number of fuel injections into the combustion chamber, wherein the first number and the second number are not the same number.
16. The apparatus of claim 15, wherein fuel injection timing is offset based at least in part on time elapsed from detection of the change from the first number to the second number of fuel injections.
17. The apparatus of claim 15, wherein the first number is greater than the second number.
18. The apparatus of claim 15, wherein the first number is less than the second number.
19. The apparatus of claim 15, wherein adjustment to fuel injection timing includes adjustment to main fuel injection timing.
20. The apparatus of claim 15, wherein adjustment to fuel injection timing includes adjustment to pilot fuel injection timing.
US10/787,991 2004-02-26 2004-02-26 Method and apparatus for adjusting fuel injection timing Expired - Lifetime US7093579B2 (en)

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US10/787,991 US7093579B2 (en) 2004-02-26 2004-02-26 Method and apparatus for adjusting fuel injection timing
CA2553876A CA2553876C (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing
PCT/US2005/004255 WO2005081806A2 (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing
CNB2005800055982A CN100451319C (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing
BRPI0508070-3A BRPI0508070A (en) 2004-02-26 2005-02-08 method and apparatus for adjusting fuel injection timing
EP05713288A EP1725753A4 (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing
KR1020067017158A KR20060129031A (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing
JP2007500857A JP2007525614A (en) 2004-02-26 2005-02-08 Method and apparatus for adjusting fuel injection timing

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050212830A1 (en) * 1999-09-17 2005-09-29 Silverbrook Research Pty Ltd Method of accessing a connection address using a mobile device with a sensing means
FR2915242A1 (en) * 2007-04-23 2008-10-24 Inst Francais Du Petrole METHOD FOR CONTROLLING COMBUSTION OF A DIESEL ENGINE
US20100231971A1 (en) * 1999-09-17 2010-09-16 Silverbrook Research Pty Ltd. Retrieving contact details using a printed medium
US20120065869A1 (en) * 2010-09-14 2012-03-15 Hyundai Motor Company System and Method for Controlling the Number of Pilot Injections
US20150046065A1 (en) * 2013-08-07 2015-02-12 Ford Global Technologies, Llc Method and system for transient fuel control

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4816651B2 (en) * 2008-01-25 2011-11-16 トヨタ自動車株式会社 Fuel injection control device for internal combustion engine
US9243580B2 (en) * 2011-12-07 2016-01-26 Ford Global Technologies, Llc Method and system for reducing soot formed by an engine
DE102013211661A1 (en) * 2012-08-03 2014-02-06 Ford Global Technologies, Llc Internal combustion engine with direct injection and reduced particulate matter emission
KR102241277B1 (en) * 2015-05-05 2021-04-15 바르실라 핀랜드 오이 A method of operating an internal combustion piston engine, a control system for controlling the operation of an internal combustion piston engine, and an internal combustion piston engine
CN109915293B (en) * 2019-03-26 2020-03-27 潍柴重机股份有限公司 Power-up time control method and control system for electric control unit pump
CN112879174B (en) * 2021-01-27 2022-12-27 东风汽车集团股份有限公司 Gasoline engine injection mode switching fuel compensation control method and system and storage medium

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6314945B1 (en) * 1999-07-28 2001-11-13 Toyota Jidosha Kabushiki Kaisha Fuel pump control apparatus
US6328018B1 (en) * 1998-06-03 2001-12-11 Keihin Corporation Control apparatus for controlling internal combustion engine
US6354269B1 (en) * 1999-09-29 2002-03-12 Mazda Motor Corporation Method and system for controlling engine
US6415762B1 (en) * 2000-07-13 2002-07-09 Caterpillar Inc. Accurate deliver of total fuel when two injection events are closely coupled
US6415655B2 (en) * 1998-03-10 2002-07-09 Robert Bosch Gmbh Method of synchronization of multi-cylinder internal combustion engine
US6476452B2 (en) * 1999-03-01 2002-11-05 Nec Corporation Bipolar/BiCMOS semiconductor device
US6536209B2 (en) * 2001-06-26 2003-03-25 Caterpillar Inc Post injections during cold operation
US6705278B2 (en) * 2001-06-26 2004-03-16 Caterpillar Inc Fuel injector with main shot and variable anchor delay
US6840211B2 (en) * 2002-11-26 2005-01-11 Isuzu Motors Limited Diesel engine
US6843222B2 (en) * 2002-12-13 2005-01-18 Robert Bosch Gmbh Method and device for starting an internal combustion engine having direct injection

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH051609A (en) 1991-06-25 1993-01-08 Toyota Motor Corp Fuel injection control device of diesel engine
JPH11173186A (en) 1997-12-05 1999-06-29 Denso Corp Device and method for controlling fuel injection rate in internal combustion engine and recording medium
EP0953756B1 (en) * 1998-04-28 2003-12-10 Toyota Jidosha Kabushiki Kaisha Fuel injection control apparatus for an internal combustion engine
ES2261388T3 (en) * 2000-03-09 2006-11-16 Robert Bosch Gmbh PROCEDURE AND DEVICE FOR CONTROLLING FUEL INJECTION IN AN INTERNAL COMBUSTION ENGINE.
JP4161529B2 (en) * 2000-10-02 2008-10-08 日産自動車株式会社 Fuel injection control device for diesel engine
JP3975717B2 (en) 2001-10-17 2007-09-12 株式会社デンソー Fuel injection control system and fuel injection control method
JP3906909B2 (en) * 2002-03-11 2007-04-18 三菱自動車工業株式会社 Split fuel injection control system

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6415655B2 (en) * 1998-03-10 2002-07-09 Robert Bosch Gmbh Method of synchronization of multi-cylinder internal combustion engine
US6328018B1 (en) * 1998-06-03 2001-12-11 Keihin Corporation Control apparatus for controlling internal combustion engine
US6476452B2 (en) * 1999-03-01 2002-11-05 Nec Corporation Bipolar/BiCMOS semiconductor device
US6314945B1 (en) * 1999-07-28 2001-11-13 Toyota Jidosha Kabushiki Kaisha Fuel pump control apparatus
US6354269B1 (en) * 1999-09-29 2002-03-12 Mazda Motor Corporation Method and system for controlling engine
US6415762B1 (en) * 2000-07-13 2002-07-09 Caterpillar Inc. Accurate deliver of total fuel when two injection events are closely coupled
US6536209B2 (en) * 2001-06-26 2003-03-25 Caterpillar Inc Post injections during cold operation
US6705278B2 (en) * 2001-06-26 2004-03-16 Caterpillar Inc Fuel injector with main shot and variable anchor delay
US6840211B2 (en) * 2002-11-26 2005-01-11 Isuzu Motors Limited Diesel engine
US6843222B2 (en) * 2002-12-13 2005-01-18 Robert Bosch Gmbh Method and device for starting an internal combustion engine having direct injection

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100231971A1 (en) * 1999-09-17 2010-09-16 Silverbrook Research Pty Ltd. Retrieving contact details using a printed medium
US8112120B2 (en) 1999-09-17 2012-02-07 Silverbrook Research Pty Ltd Contact details retrieval using a printed medium
US20110109940A1 (en) * 1999-09-17 2011-05-12 Silverbrook Research Pty Ltd Contact details retrieval using a printed medium
US20050212830A1 (en) * 1999-09-17 2005-09-29 Silverbrook Research Pty Ltd Method of accessing a connection address using a mobile device with a sensing means
WO2008142261A3 (en) * 2007-04-23 2009-02-26 Inst Francais Du Petrole Method of controlling the combustion of a diesel engine
US20100185378A1 (en) * 2007-04-23 2010-07-22 Mathieu Hillion Method of controlling the combustion of a diesel engine
WO2008142261A2 (en) * 2007-04-23 2008-11-27 Ifp Method of controlling the combustion of a diesel engine
FR2915242A1 (en) * 2007-04-23 2008-10-24 Inst Francais Du Petrole METHOD FOR CONTROLLING COMBUSTION OF A DIESEL ENGINE
US8560207B2 (en) 2007-04-23 2013-10-15 Ifp Method of controlling the combustion of a diesel engine
US20120065869A1 (en) * 2010-09-14 2012-03-15 Hyundai Motor Company System and Method for Controlling the Number of Pilot Injections
US9091225B2 (en) * 2010-09-14 2015-07-28 Hyundai Motor Company System and method for controlling the number of pilot injections
US20150046065A1 (en) * 2013-08-07 2015-02-12 Ford Global Technologies, Llc Method and system for transient fuel control
US9664125B2 (en) * 2013-08-07 2017-05-30 Ford Global Technologies, Llc Method and system for transient fuel control

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CA2553876C (en) 2012-07-17
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JP2007525614A (en) 2007-09-06
BRPI0508070A (en) 2007-07-17
WO2005081806A3 (en) 2006-04-06
EP1725753A2 (en) 2006-11-29
CA2553876A1 (en) 2005-09-09
CN1922394A (en) 2007-02-28
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CN100451319C (en) 2009-01-14
US7093579B2 (en) 2006-08-22

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